Wind Tunnel Investigation At Mach Numbers From 30 To 68 Of The Static Aerodynamic Characteristics Of Modified Mercury Exit And Escape Capsule Configurations

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Wind-tunnel Investigation at Mach Numbers from 3.0 to 6.8 of the Static Aerodynamic Characteristics of Modified Mercury Exit and Escape Capsule Configurations

Wind-tunnel Investigation at Mach Numbers from 3.0 to 6.8 of the Static Aerodynamic Characteristics of Modified Mercury Exit and Escape Capsule Configurations

Author	: Albin O. Pearson
Publisher	:
Total Pages	: 26
Release	: 1960
Genre	: Hypersonic wind tunnels
ISBN	:

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